Is the whole trailing edge of the trim tab supposed to have rivets in it, or are two of the 'rivet holes' supposed to be for water drainage?? There are two holes where it looks like rivets should be...but it look like there were never any rivets there to begin with (unblemished paint where a rivet should be, etc).
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Trim Tab Rivets
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Assuming post war aluminium tab... it is spot welded, but there were originally steel rivets of the type used on the engine baffles, filet fairings and various other assemblies, in the holes.Scott
CF-CLR Blog: http://c-fclr.blogspot.ca/
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When I rebuilt my March 1946 aircraft, I found the trailing edge of the trim tab was riveted with aluminium rivets. That may not be original of course. There were no apparent drain holes.Originally posted by Scott View PostAssuming post war aluminium tab... it is spot welded, but there were originally steel rivets of the type used on the engine baffles, filet fairings and various other assemblies, in the holes.


Last edited by Robert Lees; 01-09-2025, 09:01.
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Scott
CF-CLR Blog: http://c-fclr.blogspot.ca/
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Thanks for the replies (I really need to post a picture). There are definitely rivets in mine (post-war)...well, except in the two middle rows. It is so odd, it doesn't look like there were EVER rivets in the two side-by-side holes. The paint isn't cracked or marred in any way. Thanks for the input.
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That looks like the homemade trim I built for my clip wing. My 46 bc12d doesn't have a piano hinge. There are two small lugs welded on the elevator and the rod runs through those under the skin.Originally posted by Robert Lees View Post
When I rebuilt my March 1946 aircraft, I found the trailing edge of the trim tab was riveted with aluminium rivets. That may not be original of course. There were no apparent drain holes.


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For the file, trim tab.jpg trim tab rivets.jpg trim tab top 2.jpg attached are pics of my 1983 Ferris F21A trim tab. Simple construction with flattened and riveted trailing edge. One drain hole.
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